N14245, cancelled Mar 11, 1999

Service difficulty reports · 50

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE n_number = 'N14245' AND deregistration_id = 'N14245-1999-03-11'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR CALA9802174Accessory Unit · malfunctionedTHE NOSE GEAR GREEN LIGHT DID NOT ILLUMINATE WHEN GEAR WAS EXTENDED ON FINAL APPROACH TO EWR. THE RED LIGHT WAS ON, A MANUAL GEAR EXTENSION WAS PERFORMED DURING GO-AROUND AND THE GEAR WAS VISUALLY CHECKED THROUGH VIEW PORT. THE GREEN LIGHT ILLUMINATED ON SECDec 11, 1998 · N14245 · Boeing 7372C0 · Landing Gear Position and WarningSDR CALA9801990Battery Pack · dischargedINSPECTION FOUND THE AISLE PATH EMERGENCY LIGHTING STRIP IS INOPERATIVE FORWARD OF ROW 12 AND AFT OF ROW 20. THE BATTERY PACK WAS REMOVED AND REPLACED AND OPERATIONAL CHECKS WERE GOOD.Oct 29, 1998 · N14245 · Boeing 7372C0 · Emergency LightingSDR CALA9801802Skin · corrodedINSPECTION FOUND FUSELAGE SKIN CORRODED AT STA 294.5 BETWEEN S26L AND S27L. THE SKIN WAS REMOVED AND REPLACED IAW ECRA 5330-02708 AND ECRA 5330-02707.Sep 16, 1998 · N14245 · Boeing 7372C0 · Fuselage Main, Plate/SkinSDR CALA9801760Skin · crackedINSPECTION FOUND FORWARD GALLEY DOOR CUTOUT UPPER FORWARD CORNER CRACKED AT STA 312. THE CRACKED AREA WAS ROUTED OUT. REPAIR FILLERS, DOUBLERS, AND TRIPLERS WERE INSTALLED IAW SRM 51-30, ECRA 5330-02703 AND BOEING DRAWING 65C33800.Sep 14, 1998 · N14245 · Boeing 7372C0 · Fuselage Main, Plate/SkinSDR CALA9801759Skin · crackedINSPECTION FOUND A .5 INCH CRACK IN AFT CARGO DOOR SKIN CUTOUT AT LOWER AFT CORNER. THE EXISTING DOUBLERS WERE REMOVED, FILLERS, DOUBLERS, AND TRIPLERS WERE INSTALLED IAW SRM 51-30-2 AND ECRA 5330-02710.Sep 14, 1998 · N14245 · Boeing 7372C0 · Cargo/Baggage DoorsSDR CALA9801758Strap · puncturedINSPECTION FOUND A HOLE IN STRAP JUST FORWARD OF E & E COMPARTMENT ENTRANCE. A DOUBLER WAS INSTALLED IAW SRM 51-10-2 AND ECRA 5330-02712.Sep 14, 1998 · N14245 · Boeing 7372C0 · Fuselage Miscellaneous StructureSDR CALA9801757Doubler · corrodedINSPECTION FOUND INTERNAL DOUBLER CORRODED AT STA 294.5 LEFT. THE CORRODED SECTION OF DOUBLER WAS CUT OUT, FILLER AND DOUBLER WERE INSTALLED IAW ECRA 5330-02709.Sep 14, 1998 · N14245 · Boeing 7372C0 · Fuselage Miscellaneous StructureSDR CALA9801712Floor · crackedINSPECTION FOUND A 1 INCH CRACK AT SCREW IN FLOOR PANEL AT AFT CARGO COMPARTMENT DOOR ENTRANCE. THE FLOOR PANEL WAS REMOVED IAW SRM 51-30-2. A REPAIR WAS INSTALLED IAW SRM 51-30-2, 51-10-2, AND MM 51-20-11. THE FLOOR PANEL WAS REINSTALLED IAW SRM 51-30-2.Sep 10, 1998 · N14245 · Boeing 7372C0 · Fuselage Floor PanelSDR CALA9801711Cowl · crackedINSPECTION FOUND A 1 INCH CRACK AT FASTENER HOLE IN NR 2 ENGINE INBOARD ENGINE COWL. THE CRACKED AREA WAS CUT OUT IAW SRM 51-40-2. TWO REPAIR DOUBLERS WERE INSTALLED IAW SRM 51-40-2 AND 51-30-0.Sep 10, 1998 · N14245 · Boeing 7372C0 · Engine Cowling SystemSDR CALA9801708Skin · gougedINSPECTION FOUND LT INBOARD FOREFLAP GOUGED IN TWO PLACES AT INBOARD SIDE. THE GOUGED AREAS WERE TRIMMED OUT. AN ADHESIVE PRIMER AND BONDED FIBERGLASS REPAIR WAS INSTALLED IAW SRM 51-40-6, 51-40-9, AND MM 51-20-11.Sep 10, 1998 · N14245 · Boeing 7372C0 · Trailing Edge FlapsSDR CALA9801624Skin · corrodedINSPECTION FOUND INSIDE OF SKIN CORRODED IN LT WHEEL WELL AT STA 219.8, STRINGER 27L. THE CORROSION WAS REMOVED AND A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-10-6, 53-10-1, 53-30-3, 51-10-2, AND MM 51-11-20.Sep 3, 1998 · N14245 · Boeing 7372C0 · Fuselage Main, Plate/SkinSDR CALA9801604Angle · corrodedINSPECTION FOUND VERTICAL ANGLE CORRODED AT FS 277. THE VERTICAL ANGLE WAS REMOVED AND REPLACED IAW SRM 51-30-2.Sep 1, 1998 · N14245 · Boeing 7372C0 · Fuselage Miscellaneous StructureSDR CALA9801603Longeron · delaminatedINSPECTION FOUND NLG WHEEL WELL LONGERON 28L DELAMINATED AT BS 287. THE LONGERON WAS REMOVED AND REPLACED IAW SRM 51-30-2, 51-10-2, 51-30-2, AND MM 51-20-11.Sep 1, 1998 · N14245 · Boeing 7372C0 · Fuselage Main, Longeron/StringerSDR CALA9801602Clip · corrodedINSPECTION FOUND SHEAR CLIP CORRODED AT STA 277, LBL 17. THE SHEAR CLIP WAS REMOVED AND REPLACED IAW SRM 53-10-2 AND 51-30-2.Aug 31, 1998 · N14245 · Boeing 7372C0 · Fuselage Miscellaneous StructureSDR CALA9801583Stiffener · crackedINSPECTION FOUND A 2 INCH CRACK AT LOWER ATTACH POINT OF VERTICAL STIFFENER AT AFT CARGO FORWARD PRESSURE BULKHEAD STA 727, LBL 18. THE STIFFENER WAS REMOVED AND A NEW STIFFENER WAS INSTALLED IAW SRM 51-30-2.Aug 28, 1998 · N14245 · Boeing 7372C0 · Fuselage Main, Longeron/StringerSDR CALA9801569Angle · corrodedINSPECTION FOUND ANGLE CORRODED AT STA 294.5 TO 325.38, LBL 8. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-30-2 AND 51-30-5.Aug 27, 1998 · N14245 · Boeing 7372C0 · Fuselage Miscellaneous StructureSDR CALA9801536Skin · crackedINSPECTION FOUND A .0625 AND 1.5 INCH CRACK IN FUSELAGE SKIN DOUBLER FORWARD OF COCKPIT WINDOW AT STA 178, BL 0. THE SKIN DOUBLER WAS REMOVED IAW SRM 51-30-2. REPAIR PARTS WERE INSTALLED IAW SRM 51-30-2 AND ECRA 5310-03754.Aug 25, 1998 · N14245 · Boeing 7372C0 · Fuselage Main, Plate/SkinSDR CALA9801535Floorbeam · crackedINSPECTION FOUND A 2 INCH CRACK IN FLOORBEAM LOWER CHORD AT STA 675, BBL 0.07. THE LOWER CHORD WAS REMOVED AND A NEW LOWER CHORD ANGLE AND TWO REINFORCING SPLICE ANGLES WERE INSTALLED IAW ECRA 5710-01929.Aug 25, 1998 · N14245 · Boeing 7372C0 · Fuselage Main, Floor BeamSDR CALA9801523Angle · crackedINSPECTION FOUND A 3 INCH CRACK IN LT FORWARD WING TO BODY FAIRING ATTACH ANGLE. THE ANGLE WAS REMOVED AND A REPAIR ANGLE WAS INSTALLED IAW ECRA 5350-01227 AND 51-30-2.Aug 25, 1998 · N14245 · Boeing 7372C0 · Fuselage Miscellaneous StructureSDR CALA9801522Floorbeam · crackedINSPECTION FOUND A 1 INCH CRACK IN FLOORBEAM WEB AT STA 663, BL 0. A REPAIR WAS INSTALLED IAW ECRA 5710-01931.Aug 25, 1998 · N14245 · Boeing 7372C0 · Fuselage Main, Floor BeamSDR CALA9801489Casting · crackedINSPECTION FOUND NR 1 ENGINE PYLON PANEL LOWER SIDE NUT PLATE AREA CRACKED AND FOUND A 1 CRACK IN INBOARD FORWARD ATTACH CASTING. THE CASTING WAS REMOVED IAW SRM 51-30-2. A REPAIR ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-40-3, 51-10-2, AND MM 51-20-11. Aug 19, 1998 · N14245 · Boeing 7372C0 · Nacelle/Pylon StructureSDR CALA9801482Rib · gougedINSPECTION FOUND A GOUGE IN LT WING LEADING EDGE RIB INBOARD OF NR 3 SLAT. A REPAIR ANGLE DOUBLER AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 51-40-3, 51-10-2, 51-30-2, AND MM 51-21-31.Aug 18, 1998 · N14245 · Boeing 7372C0 · Wing, Rib/BulkheadSDR CALA9801468Angle · crackedINSPECTION FOUND A .5 INCH CRACK IN FORWARD ANGLE IN AFT CARGO COMPARTMENT AT STA 727, BL 0, STRINGER 29L. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-30-2.Aug 15, 1998 · N14245 · Boeing 7372C0 · Fuselage Miscellaneous StructureSDR CALA9801466Fairing · crackedINSPECTION FOUND A 1 INCH CRACK ON NR 1 ENGINE WING TO ENGINE UPPER FAIRING AT LOWER INBOARD CORNER, WS 183.4. THE CRACK WAS STOP DRILLED, AN EXTERNAL REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 54-30-2, FIGURE 2, 51-40-2, FIGURE 1, AND 51-30-2.Aug 15, 1998 · N14245 · Boeing 7372C0 · Nacelle/Pylon StructureSDR CALA9801465Fairing · crackedINSPECTION FOUND A 1 INCH CRACK AT FASTENER HOLE ON NR 1 ENGINE WING TO ENGINE UPPER FAIRING AT LOWER INBOARD CORNER, WS 181.0. THE CRACK WAS STOP DRILLED, AN EXTERNAL REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 54-30-2, FIGURE 2 AND 51-40-2, FIGURE 1Aug 15, 1998 · N14245 · Boeing 7372C0 · Nacelle/Pylon StructureSDR CALA9801464Longeron · crackedINSPECTION FOUND A 2.5 INCH CRACK ON END CAP (LONGERON) PANEL NR 2 ENGINE FAIRING. THE LONGERON WAS REMOVED AND A NEW LONGERON WAS INSTALLED IAW SRM 51-30-2.Aug 15, 1998 · N14245 · Boeing 7372C0 · Nacelle/Pylon, Longeron/StringerSDR CALA9801463Fairing · chafedINSPECTION FOUND A HOLE CHAFED THROUGH NR 1 ENGINE THRUST REVERSER EXTENSION UPPER CLOSE OUT FAIRING. THE AREA WAS REPAIRED IAW SRM 51-20-1, FIGURE 7.Aug 15, 1998 · N14245 · Boeing 7372C0 · Engine Thrust ReverserSDR CALA9801081Tat Indicator · shortedTHE TAT CIRCUIT BREAKER POPPED FOLLOWED BY SMOKE IN THE COCKPIT AFTER TAKEOFF. THE SMOKE APPEARED TO COME FROM THE TAT GUAGE. THE AIRCRAFT WAS RETURNED TO ATL WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE TAT INDICATOR AT FAULT. THE INDICATOR WASJun 16, 1998 · N14245 · Boeing 7372C0 · Outside Air Temperature Indicator/SensorSDR CALA9800903Web · crackedINSPECTION FOUND A 2 INCH CRACK IN SHEAR BEAM WEB IN LT WHEEL WELL AT STA 727. REPAIRED IAW DRAWING 65C29228.May 27, 1998 · N14245 · Boeing 7372C0 · Fuselage Miscellaneous StructureSDR CALA9800415Circuit Breaker · inoperativeTHE LANDING GEAR HANDLE COULD NOT BE RAISED PAST THE OFF POSITION AFTER TAKEOFF FROM MSY. THE GEAR LIGHTS CIRCUIT BREAKER WAS FOUND POPPED. THE CIRCUIT BREAKER WAS RESET AND THE GEAR RAISED NORMALLY. A FEW MINUTES LATER THE LIGHTS CIRCUIT BREAKER POPPED AGAMar 12, 1998 · N14245 · Boeing 7372C0 · Landing Gear SelectorSDR CALA9800391Fire Loop · chafedTHE NR 2 ENG FIRE WARNING LIGHT AND BELL ACTIVATED BRIEFLY SEVERAL TIMES IN FLIGHT. THE DURATION OF EACH WARNING WAS LESS THAN ONE SECOND. THE NR 2 ENG FIRE LIGHT AND WARNING BELL CAME ON STEADY AFTER LANDING AT CLE. BOTH FIRE BOTTLES WERE DISCHARGED, AND SMar 5, 1998 · N14245 · Boeing 7372C0 · Fire DetectionSDR CALA9700859Web · crackedINSPECTION FOUND A .5 INCH CRACK AT LIGHTENING HOLE OF WEB, STA 360 JUST ABOVE STRINGER 17L. THE WEB WAS REMOVED AND A NEW WEB WAS FABRICATED AND INSTALLED IAW SRM 51-10-6 AND 51-10-1.May 24, 1997 · N14245 · Boeing 7372C0 · Fuselage Miscellaneous StructureSDR CALA9700858Support · corrodedINSPECTION FOUND AFT CLOSET FLOOR SUPPORT CORRODED AT FS 1010, RBL 17.0 TO RBL 46.5. THE FLOOR SUPPORT WAS REMOVED, A FLOOR SUPPORT AND HAT CHANNEL WERE FABRICATED AND INSTALLED IAW SRM 51-10-1, 51-10-6, AND 51-30-2.May 19, 1997 · N14245 · Boeing 7372C0 · Fuselage Miscellaneous StructureSDR CALA9700764Web · corrodedINSPECTION FOUND CABIN FLOOR WEB CORRODED AT STA 1016 RBL 15. THE CORRODED AREA WAS CUT OUT, A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-40-2.May 15, 1997 · N14245 · Boeing 7372C0 · Fuselage Miscellaneous StructureSDR CALA9700762Web · corrodedINSPECTION FOUND CABIN FLOOR WEB CORRODED AT STA 1016 RBL 30 TO 36. THE CORROSION WAS REMOVED AND A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-00-6, 51-30-8, AND 51-40-3.May 15, 1997 · N14245 · Boeing 7372C0 · Fuselage Miscellaneous StructureSDR CALA9700761Floorbeam · corrodedINSPECTION FOUND MAIN DECK FLOORBEAM CORRODED AT FS 520 LBL 24.5. NEW DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 51-30-2 AND 51-10-6.May 14, 1997 · N14245 · Boeing 7372C0 · Fuselage Main, Floor BeamSDR CALA9700760Floor Support · corrodedINSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 328 TO 344 RBL 12. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 53-10-2.May 14, 1997 · N14245 · Boeing 7372C0 · Fuselage Miscellaneous StructureSDR CALA9700759Strap · corrodedINSPECTION FOUND AFT LAV FLOOR WEB STRAP CORRODED AT STA 1006 TO 1024 LBL 28. THE STRAP WAS REMOVED AND A NEW PART WAS FABRICATED AND INSTALLED IAW SRM 51-30-2, 53-10-2, 51-10-2.May 14, 1997 · N14245 · Boeing 7372C0 · Fuselage Miscellaneous StructureSDR CALA9700758Intercostal · crackedINSPECTION FOUND A 2 INCH CRACK IN INTERCOSTAL BETWEEN FS 303.9 AND 294.5 AT STRINGER 15L. A NEW INTERCOSTAL WAS FABRICATED AND INSTALLED IAW SRM 51-30-2, 53-10-1, 51-10-2.May 13, 1997 · N14245 · Boeing 7372C0 · Fuselage Miscellaneous StructureSDR CALA9700757Floor Support · corrodedINSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 312 LBL 12. THE SUPPORT WAS REMOVED AND A NEW SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 53-10-2, FIGURE 7, 51-20-0 AND 51-10-2.May 13, 1997 · N14245 · Boeing 7372C0 · Fuselage Miscellaneous StructureSDR CALA9700755Skin · dentedINSPECTION FOUND, FUSELAGE SKIN DENTED AT STA 940, LONGERON 20L. THE DENTED AREA WAS CUTOUT AND A DOUBLER REPAIR WAS INSTALLED IAW SRM 53-30-3, FIGURE 6.May 12, 1997 · N14245 · Boeing 7372C0 · Fuselage Main, Plate/SkinSDR CALA9700763Skin · corrodedINSPECTION FOUND LT FUSELAGE SKIN CORRODED AT STA 410, STRINGER 16L. THE SKIN WAS REMOVED, A DOUBLER WAS FABRICATED IAW SRM 53-30-3, FIGURE 6 AND 53-30-3, FIGURE 6 SHEET 4.May 11, 1997 · N14245 · Boeing 7372C0 · Fuselage Main, Plate/SkinSDR CALA9700756Intercostal · crackedINSPECTION FOUND A.75 INCH CRACK IN MAIN DECK FLOOR INTERCOSTAL AT FS 520, LBL 24.5. THE CRACK WAS STOP DRILLED, A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-10-01, 51-40-2, FIGURE 1 AND 51-30-2.May 8, 1997 · N14245 · Boeing 7372C0 · Fuselage Miscellaneous StructureSDR CALA9601322Solenoid Valve · malfunctionedTHE AIRCRAFT BECAME HARD TO CONTROL ABOUT THE VERTICAL AXIS WHILE ON FINAL APPROACH. THE AIRCRAFT WANTED TO DUTCH ROLL AND YAW EXCESSIVELY AND DIDN'T RESPOND EFFECTIVELY TO PILOT CONTROLLED INPUTS ON RUDDER. THE AIRCRAFT HANDLED THE SAME WITH AND WITHOUT YAWSep 22, 1996 · N14245 · Boeing 7372C0 · Rudder Control SystemSDR CALA9601057Fitting · crackedINSPECTION FOUND A CRACK IN VERTICAL LEG OF FORWARD HALF OF LOWER LT FITTING AT B.S. 695, STRINGER 18A. THE CRACKED FITTING WAS REMOVED AND A NEW FITTING WAS INSTALLED IAW DRAWING NR 65C34490 AND SA008-5310-02456 THROUGH SA0013-5310-02456.Jul 11, 1996 · N14245 · Boeing 7372C0 · Fuselage Miscellaneous StructureSDR CALA9601061Skin · corrodedINSPECTION FOUND FUSELAGE SKIN CORRODED AT OUTFLOW VALVE. THE CORRODED SECTION OF SKIN WAS CUT OUT. FILLER AND DOUBLER WERE FABRICATED AND INSTALLED IAW SRM'S 53-30-3, 51-10-6, AND 51-10-2.Jul 10, 1996 · N14245 · Boeing 7372C0 · Fuselage Main, Plate/SkinSDR CALA9601060Skin · corrodedINSPECTION FOUND FUSELAGE SKIN CORRODED JUST AFT OF AFT CARGO DOOR AFT LOWER CORNER. THE CORRODED SECTION OF SKIN WAS CUT OUT. FILLER AND SPLICE DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 53-30-3 AND SRM 51-30-2.Jul 10, 1996 · N14245 · Boeing 7372C0 · Fuselage Main, Plate/SkinSDR CALA9601059Bulkhead Web · crackedINSPECTION FOUND A 7 INCH CRACK IN PRESSURE BULKHEAD WEB AT WL 218, STA 178 ON BOTH LT AND RT SIDES. BOTH CRACKED AREAS OF BULKHEAD WEB WERE CUT OUT. FILLER AND DOUBLER REPAIRS WERE FABRICATED AND INSTALLED IAW SRM'S 53-10-2, 51-10-2, AND 51-30-2.Jul 10, 1996 · N14245 · Boeing 7372C0 · Fuselage Main, BulkheadSDR CALA9601058Chord · crackedINSPECTION FOUND A CRACK PAST SECOND FASTENER HOLE OF CHORD AT STRINGER 18A ON BOTH THE LT AND RT SIDES OF B.S. 727. THE CHORD SEGMENTS WERE REMOVED AND REPLACED IAW BOEING DRAWING 65C33722 AND CAL WORK CARD 15-5310-1-0023.Jul 10, 1996 · N14245 · Boeing 7372C0 · Fuselage Miscellaneous StructureSDR CAL950597Hyd Line · leakingEWR - FLT 1216 - THE A-SYSTEM HYDRAULIC FLUID DROPPED IN-FLIGHT. THE NR 2 A-HYDRAULIC PUMP WAS TURNED OFF AND THE QUANTITY WAS MAINTAINED AT THREE-FOURTHS GALLON WITH PRESSURE HOLDING. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND AN A-SYSTEM HYDRJul 17, 1995 · N14245 · Boeing 7372C0 · Hydraulic System, Main
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